US20190041170A1 - Modular man-portable drone barrier - Google Patents
Modular man-portable drone barrier Download PDFInfo
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- US20190041170A1 US20190041170A1 US15/928,318 US201815928318A US2019041170A1 US 20190041170 A1 US20190041170 A1 US 20190041170A1 US 201815928318 A US201815928318 A US 201815928318A US 2019041170 A1 US2019041170 A1 US 2019041170A1
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- 230000004888 barrier function Effects 0.000 title claims abstract description 76
- 238000000034 method Methods 0.000 claims description 9
- 238000004873 anchoring Methods 0.000 claims description 4
- 239000000463 material Substances 0.000 description 10
- 230000000712 assembly Effects 0.000 description 7
- 238000000429 assembly Methods 0.000 description 7
- 230000007246 mechanism Effects 0.000 description 7
- 239000007789 gas Substances 0.000 description 5
- 239000001307 helium Substances 0.000 description 4
- 229910052734 helium Inorganic materials 0.000 description 4
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 150000002431 hydrogen Chemical class 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
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- 229920002799 BoPET Polymers 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 239000005041 Mylar™ Substances 0.000 description 1
- 229920010741 Ultra High Molecular Weight Polyethylene (UHMWPE) Polymers 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000008676 import Effects 0.000 description 1
- 229920000785 ultra high molecular weight polyethylene Polymers 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Arresting gear; Liquid barriers
- B64F1/027—Arresting gear; Liquid barriers using net or mesh
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Arresting gear; Liquid barriers
- B64F1/0295—Arresting gear; Liquid barriers aerodynamically or aerostatically supported, e.g. parafoil or balloon
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
- F41H11/04—Aerial barrages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
Definitions
- the present invention relates generally to barriers.
- UAV unmanned aerial vehicle
- drone is an aircraft without a human pilot aboard.
- many drones available today are much smaller and cheaper, and are widely used for civilian purposes by hobbyists and the like.
- an aerial vehicle barrier comprises two or more balloons selectively inflatable with a lighter-than-air gas, two or more flexible trunk lines, two or more flexible branch lines, and two or more connecting lines.
- Each trunk line has a ground-anchorable end and an opposite end attached or selectively attachable to a respective one of the balloons.
- Each branch line has opposing ends attached or selectively attachable to respective ones of two adjacent trunk lines to span between the two adjacent trunk lines.
- Each connecting line has opposing ends attached to respective ones of two adjacent branch lines.
- Some or all of the connecting lines may be flexible.
- the barrier may further comprise two or more flexible hanging lines, each hanging line having a first end attached to a respective branch line and an opposing unattached end.
- the two or more flexible hanging lines may comprise flexible hanging lines having two or more different lengths.
- Each branch line may comprise first and second branch line portions.
- Each branch line portion may have a proximal end and a distal end. The proximal end of each branch line portion may be attached or selectively attachable to a respective one of the trunk lines. The distal end of each first branch line portion may be attached or selectively attachable to the distal end of a respective one of the second branch line portions.
- an aerial vehicle barrier comprises two or more flexible trunk lines, two or more flexible branch lines, two or more connecting lines, and two or more flexible hanging lines.
- Each trunk line has a first ground-anchorable end and an opposite second end adapted to be supported above a ground surface.
- Each branch line has opposing ends attached or selectively attachable to respective ones of two adjacent trunk lines to span between the two adjacent trunk lines.
- Each connecting line has opposing ends attached to respective ones of two adjacent branch lines.
- Each hanging line has a first end attached to a respective branch line and an opposing unattached end.
- a method of creating a barrier to an aerial vehicle comprises (a) obtaining a barrier device as described herein; (b) anchoring the first end of each of the trunk lines of the barrier device to a ground surface at a desired distance from each adjacent trunk line; and (c) inflating the balloons of the barrier device with a lighter-than-air gas such that the barrier device is lifted upward to a height determined by a length of the trunk lines.
- FIG. 1 is a simplified side view of a man-portable drone barrier, in accordance with embodiments of the present invention.
- Embodiments of the invention are directed to a man-portable drone barrier system comprising modular components that are easily transported to any desired location, quickly assembled with minimal tools, and raised to a desired height via helium balloons (or any other suitable lifting device(s) or method(s)). Once assembled and raised, the system creates a mesh fence in the air to entrap and/or entangle a drone that flies into or near the barrier.
- Barrier system 10 comprises a first barrier assembly 12 a and a second barrier assembly 12 b.
- the first and second barrier assemblies are assembled together as described below to form a complete barrier system. While two barrier assemblies are shown and described herein, more than two assemblies could be assembled together (as described further below) in a modular fashion to form a wider barrier if desired.
- Each barrier assembly 12 a, 12 b may be individually and separately packaged for ease and clarity of layout and assembly.
- the overall weight is low enough and unassembled size of the system is small enough to enable the system to be readily man-portable (i.e., capable of being carried by one person).
- the first barrier assembly 12 a comprises a main trunk line 16 a affixed at one end (via connection point 40 a ) to a lighter-than-air object, such as a balloon 14 a inflated with a lighter-than-air gas such as helium or hydrogen, and at the other end (via connection point 42 a ) to a securing device 18 a for anchoring or securing the assembly 12 a to the ground (or to any other suitable fixed object), such as a ground stake, sandbag (or other similar weighted object), clamp, hook, carabiner, tie-off, or the like.
- a lighter-than-air object such as a balloon 14 a inflated with a lighter-than-air gas such as helium or hydrogen
- a securing device 18 a for anchoring or securing the assembly 12 a to the ground (or to any other suitable fixed object), such as a ground stake, sandbag (or other similar weighted object), clamp, hook, carabiner,
- the main trunk line 16 a may be permanently affixed to the balloon 14 a, or may be removably affixed to the balloon 14 a such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation).
- the main trunk line 16 a may be permanently affixed to the securing device 18 a, or may be removably affixed to the securing device 18 a such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation).
- the second barrier assembly 12 b comprises a main trunk line 16 b affixed at one end (via connection point 40 b ) to a lighter-than-air object, such as a balloon 14 b inflated with a lighter-than-air gas such as helium or hydrogen, and at the other end (via connection point 42 b ) to a securing device 18 b for anchoring or securing the assembly 12 b to the ground (or to any other suitable fixed object), such as a ground stake, sandbag (or other similar weighted object), clamp, hook, carabiner, tie-off, or the like.
- a lighter-than-air object such as a balloon 14 b inflated with a lighter-than-air gas such as helium or hydrogen
- a securing device 18 b for anchoring or securing the assembly 12 b to the ground (or to any other suitable fixed object), such as a ground stake, sandbag (or other similar weighted object), clamp, hook, carabiner,
- the main trunk line 16 b may be permanently affixed to the balloon 14 b, or may be removably affixed to the balloon 14 b such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation).
- the main trunk line 16 b may be permanently affixed to the securing device 18 b, or may be removably affixed to the securing device 18 b such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation).
- the balloons 14 a, 14 b may be any suitable, strong, durable material (such as Mylar) that can be inflated as needed with a lighter-than-air gas in a variety of locations and situations and which is large enough to lift each assembly 12 a, 12 b to the height allowed by the length of each main trunk line 16 a, 16 b.
- the balloons may be replaced with any suitable flying or lifting device, such as hovering drones.
- the main trunk lines 16 a, 16 b may be constructed of any elongated material, such as wire, cable, rope, etc., that is durable, flexible, and strong enough to withstand the upward pull of the balloons and support the branch lines and sub-branch lines (described below), yet light enough to be held aloft by the balloons (along with the other components described below).
- the material may be braided or monofilament, or any other suitable construction that provides the desired strength-to-weight ratio.
- the main trunk lines 16 a, 16 b may be of any suitable, desired length. In one exemplary embodiment of the invention, the main trunk lines 16 a, 16 b are about 200 feet long.
- the main trunk lines 16 a, 16 b may be adapted to attach to the balloons 14 a, 14 b and the securing devices 18 a, 18 b only at the ends of the main trunk lines 16 a, 16 b.
- the main trunk lines 16 a, 16 b may be adapted to attach to the balloons 14 a, 14 b and/or the securing devices 18 a, 18 b at two or more different locations along the lengths of the main trunk lines 16 a, 16 b.
- the barrier may be configured to be held aloft at a variety of different heights.
- the first barrier assembly 12 a further comprises one or more (three are illustrated) branch lines 20 a affixed to the left side of the main trunk line 16 a in a spaced-apart configuration and one or more (three are illustrated) branch lines 20 a affixed to the right side of the main trunk line 16 a in a spaced-apart configuration.
- the left-side branch lines (and sub-branch lines, described below) of the first barrier assembly 12 a are typically (but not necessarily) identical to the right-side branch lines and sub-branch lines of the first barrier assembly 12 a, and are not fully illustrated for simplicity.
- the left-side branch lines (and sub-branch lines) of the first barrier assembly 12 a may be omitted if main trunk line 16 a is to be the leftmost end of the barrier.
- the left-side and right-side branch and sub-branch lines of a given barrier assembly will be identical.
- the branch lines 20 a typically begin near the top end of the main trunk line 16 a (i.e., near the balloon 14 a ) and extend lower at regular intervals until they reach a point at or near the connection between the main trunk line and the securing device, 18 a.
- Each branch line 20 a is affixed to the main trunk line 16 a at a connection point 22 a.
- Each branch line 20 a may be permanently affixed to the main trunk line 16 a, or may be removably affixed to the main trunk line 16 a such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation including the simple tying of the branch line to the trunk line).
- the branch lines 20 a should be spaced close enough together for it to be unlikely that a drone could pass through the barrier, but far enough apart to provide the desired overall height of the barrier. In one exemplary embodiment of the invention, the branch lines 20 a are spaced about eighteen inches apart.
- the second barrier assembly 12 b further comprises one or more (three are illustrated) branch lines 20 b affixed to the left side of the main trunk line 16 b in a spaced-apart configuration and one or more (three are illustrated) branch lines 20 a affixed to the right side of the main trunk line 16 a in a spaced-apart configuration.
- the left-side branch lines (and sub-branch lines, described below) of the second barrier assembly 12 b are typically (but not necessarily) identical to the right-side branch lines and sub-branch lines of the second barrier assembly 12 b, and are not fully illustrated for simplicity.
- the right-side branch lines (and sub-branch lines) of the second barrier assembly 12 b may be omitted if main trunk line 16 b is to be the rightmost end of the barrier.
- the branch lines 20 b are typically located near the top end of the main trunk line 16 b (i.e., near the balloon 14 b ) and extend lower at regular intervals until they reach a point at or near the connection between the main trunk line and the securing device, 18 b.
- Each branch line 20 b is affixed to the main trunk line 16 b at a connection point 22 b.
- This connection point could be integral to the main trunk line as depicted or could be affixed with a clamp or simply by tying the branch line to the main trunk line.
- Each branch line 20 b may be permanently affixed to the main trunk line 16 b, or may be removably affixed to the main trunk line 16 b such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation including the simple tying of the branch line to the trunk line).
- the branch lines 20 b should be spaced close enough together for it to be unlikely that a drone could pass through the barrier, but far enough apart to provide the desired overall height of the barrier. In one exemplary embodiment of the invention, the branch lines 20 b are spaced about eighteen inches apart.
- the branch lines 20 a, 20 b may be constructed of any elongated material, such as wire, cable, rope, etc., that is durable, flexible, strong enough to withstand the tension as the trunk lines move and support the sub-branch lines (described below) and to withstand the impact of a drone, yet light enough to be held aloft by the balloons (along with the other components).
- the material may be braided or monofilament, or any other suitable construction that provides the desired strength-to-weight ratio.
- the branch lines 20 a, 20 b do not need to be a strong as the trunk lines 16 a, 16 b, so the branch lines 20 a, 20 b will typically be thinner and lighter than the trunk lines 16 a, 16 b.
- the branch lines 20 a, 20 b may be of any suitable, desired length. In one exemplary embodiment of the invention, the branch lines 20 a, 20 b are about ten feet long. The placement of the trunk lines 16 a, 16 b (i.e., the distance apart) is based on the length of the branch lines 20 a, 20 b (so the trunk lines 16 a, 16 b would be about twenty feet apart in such an exemplary embodiment).
- the distal end of one right-side branch line 20 a of the first assembly 12 a is affixed to the distal end of a corresponding left-side branch line 20 b of the second assembly 12 b at connection point 24 .
- the affixation of the distal ends is performed for each pair of corresponding branch lines from the right-side of the first assembly 12 a and the left-side of the second assembly 12 b.
- the distal ends of the corresponding branch lines 20 a, 20 b are removably affixed, such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation including by means of a simple clamp or simply tying the two distal ends together), such that the barrier system 10 comprising any desired number of assemblies 12 a, 12 b can be readily assembled and disassembled as needed.
- barrier assemblies may be assembled together.
- a third barrier assembly (not illustrated) may be connected to the first barrier assembly 12 a on the opposite side from the second barrier assembly 12 b.
- the right-side branch lines of the third assembly are affixed to the corresponding left-side branch lines 20 a of the first assembly 12 a.
- a fourth barrier assembly (not illustrated) may be connected to the second barrier assembly 12 b on the opposite side from the first barrier assembly 12 a.
- the left-side branch lines of the fourth assembly are affixed to the corresponding right-side branch lines 20 a of the second assembly 12 b.
- barrier systems may be connected together as described to form a barrier system of a desired length.
- the branch lines that are not affixed to an adjacent assembly's branch lines may simply hang down.
- the branch lines that are not affixed to an adjacent assembly's branch lines may be removed.
- the first barrier assembly 12 a may further comprise one or more (six are illustrated) complete sub-branch lines 26 a and/or one or more partial sub-branch lines 28 a.
- Each complete sub-branch line 26 a is affixed (permanently or removably) at opposing ends to adjacent branch lines 20 a, and together with the branch lines 20 a form a grid and help maintain the spacing between the branch lines 20 a.
- each partial sub-branch line 28 a is affixed (permanently or removably) at one end to a corresponding branch line, such that the opposing end is free and the partial sub-branch line 28 a swings freely. Because the partial sub-branch lines are affixed at only one end to a corresponding branch line, the partial sub-branch lines may also be termed “hanging lines.”
- the second barrier assembly 12 b may further comprise one or more (six are illustrated) complete sub-branch lines 26 b and/or one or more partial sub-branch lines 28 b.
- Each complete sub-branch line 26 b is affixed (permanently or removably) at opposing ends to adjacent branch lines 20 b, and together with the branch lines 20 b form a grid and help maintain the spacing between the branch lines 20 b.
- Each partial sub-branch line 28 b is affixed (permanently or removably) at one end to a corresponding branch line, such that the opposing end is free and the partial sub-branch line 28 b swings freely.
- Each grid formed by the branch lines and the complete sub-branch lines and main trunk lines will typically have at least one and typically more than one partial sub-branch line positioned within the grid.
- most of the grids have one partial sub-branch line each and two of the grids have three sub-branch lines each. Any suitable number of partial sub-branch lines may be positioned within each grid, with any suitable spacing.
- one ore more partial sub-branch lines 30 a, 30 b may hang down from the bottommost branch line (such that they may not technically be positioned within a grid).
- the partial sub-branch lines would be extremely light weight but high modulus (such as monofilament) such that they would entangle drone rotors either through gravity or by being pulled into the drone rotors through updraft (one of the partial sub-branch lines 28 a is shown pulled upward as if by updraft).
- the complete sub-branch line 26 a, 26 b and the partial sub-branch lines 28 a, 28 b may be constructed of any elongated material, such as wire, cable, rope, etc., that is durable, flexible, strong enough to withstand the tension as the branch lines move and to withstand the impact of a drone, yet light enough to be held aloft by the balloons (along with the other components).
- the material may be braided or monofilament, or any other suitable construction that provides the desired strength-to-weight ratio.
- the complete and partial sub-branch lines 26 a, 26 b, 28 a, 28 b do not need to be a strong as the branch lines 20 a, 20 b, so the complete and partial sub-branch lines 26 a, 26 b, 28 a, 28 b will typically be thinner and lighter than the branch lines 20 a, 20 b.
- the complete sub-branch lines 26 a, 26 b may be constructed of a rigid or semi-rigid material to help maintain the spacing between the branch lines 20 a, 20 b.
- the complete sub-branch lines 26 a, 26 b should be spaced close enough together for it to be unlikely that a drone could pass through the barrier. In one exemplary embodiment of the invention, the complete sub-branch lines 26 a, 26 b are spaced about eighteen inches apart.
- the partial sub-branch lines 28 a, 28 b may be of any suitable, desired length. In one exemplary embodiment of the invention, the partial sub-branch lines 28 a, 28 b are about ten inches long.
- the length of the complete sub-branch lines 26 a, 26 b is based on the spacing of the branch lines 20 a, 20 b.
- the partial sub-branch lines may be all uniform in length, or may be of variable length. In FIG. 1 , most of the partial sub-branch lines are the same length, but two of the grids are shown with three sub-branch lines each (including partial sub-branch lines 32 a, 32 b that are long enough to reach or nearly reach the next lower branch line).
- the free-swinging partial sub-branch lines 28 a, 28 b provide a potential entanglement for any drone that flies too close to the barrier.
- the free ends of a partial sub-branch line 28 a, 28 b can be caught in a drone's updraft (this is illustrated in FIG. 1 in the top right partial sub-branch 28 a of the first assembly 12 a ) and advantageously become entangled in one or more of the drone's rotors, thereby potentially disabling the drone.
- the balloons 14 , 14 b are inflated with a helium or hydrogen.
- the inflated balloons will rise to a height permitted by the length of the main trunk lines 16 a, 16 b, and assume a generally upright orientation (although wind will often move the balloons 14 a, 14 b and tilt the main trunk lines 16 a, 16 b.
- the affixed branch lines 20 a, 20 b will span between the main trunk lines 16 a, 16 b and assume a generally horizontal orientation.
- the top portion of the main trunk lines 16 a, 16 b (i.e., the portion to which the branch lines are attached), the branch lines 20 a, 20 b, and the complete sub-branch lines 26 a, 26 b form a substantially upright grid suspended a desired height in the air to form a barrier to a drone that might directly contact one or more of the main trunk lines 16 a, 16 b, the branch liens 20 a, 20 b, and/or the complete sub-branch lines 26 a, 26 b, or may become entangled by one or more of the partial sub-branch lines 28 a, 28 b, 30 a, 30 b, 32 a, 32 b.
- wind, convection or other environmental conditions may disperse the sub-branch lines in a broader area, increasingly the likelihood of drone entanglement.
- the trunk lines, branch lines, and complete sub-branch lines are made from AmSteel Blue rope from Samson Rope Technologies, Inc. which is made of Dyneema ultra-high-molecular-weight polyethylene (UHMWPE).
- the trunk is 5/32′′ diameter with a 4000 pound (lb.) average strength, and the branches are 7/64′′ diameter with a 1600 lb. average strength.
- the partial sub-branch lines are made of 25 lb. monofilament fishing line from Ande, Inc.
Abstract
Description
- This application claims priority to pending U.S. Provisional Application Ser. No. 62/539,608, filed Aug. 1, 2017, the contents of which are incorporated herein by reference in its entirety.
- The present invention relates generally to barriers.
- An unmanned aerial vehicle (UAV) or drone is an aircraft without a human pilot aboard. Initially developed as large, sophisticated aircraft for use by the military, many drones available today (such as quadcopters) are much smaller and cheaper, and are widely used for civilian purposes by hobbyists and the like.
- Unfortunately, the ease of use and wide availability of such civilian drones enables terrorists and other saboteurs to use these drones for nefarious purposes. The drones may be fitted with explosives, or simply flown into critical equipment. Recent military action in the Middle East indicates that terrorist use small drones to distract, threaten, and kill military forces. These events present the need for a simple, man-portable barrier that professional soldiers could quickly and easily construct using few or no tools in combat conditions.
- In one embodiment of the invention, an aerial vehicle barrier comprises two or more balloons selectively inflatable with a lighter-than-air gas, two or more flexible trunk lines, two or more flexible branch lines, and two or more connecting lines. Each trunk line has a ground-anchorable end and an opposite end attached or selectively attachable to a respective one of the balloons. Each branch line has opposing ends attached or selectively attachable to respective ones of two adjacent trunk lines to span between the two adjacent trunk lines. Each connecting line has opposing ends attached to respective ones of two adjacent branch lines.
- Some or all of the connecting lines may be flexible.
- The barrier may further comprise two or more flexible hanging lines, each hanging line having a first end attached to a respective branch line and an opposing unattached end. The two or more flexible hanging lines may comprise flexible hanging lines having two or more different lengths.
- Each branch line may comprise first and second branch line portions. Each branch line portion may have a proximal end and a distal end. The proximal end of each branch line portion may be attached or selectively attachable to a respective one of the trunk lines. The distal end of each first branch line portion may be attached or selectively attachable to the distal end of a respective one of the second branch line portions.
- In an alternative embodiment of the invention, an aerial vehicle barrier comprises two or more flexible trunk lines, two or more flexible branch lines, two or more connecting lines, and two or more flexible hanging lines. Each trunk line has a first ground-anchorable end and an opposite second end adapted to be supported above a ground surface. Each branch line has opposing ends attached or selectively attachable to respective ones of two adjacent trunk lines to span between the two adjacent trunk lines. Each connecting line has opposing ends attached to respective ones of two adjacent branch lines. Each hanging line has a first end attached to a respective branch line and an opposing unattached end. Some or all of the connecting lines may be flexible.
- In another alternative embodiment of the invention, a method of creating a barrier to an aerial vehicle comprises (a) obtaining a barrier device as described herein; (b) anchoring the first end of each of the trunk lines of the barrier device to a ground surface at a desired distance from each adjacent trunk line; and (c) inflating the balloons of the barrier device with a lighter-than-air gas such that the barrier device is lifted upward to a height determined by a length of the trunk lines.
- Reference will now be made to the accompanying drawings, which are not necessarily drawn to scale. The following detailed description of the disclosure will be better understood when read in conjunction with the appended drawings. It should be understood, however, that the disclosure is not limited to the precise arrangements and instrumentalities shown. In the drawings:
-
FIG. 1 is a simplified side view of a man-portable drone barrier, in accordance with embodiments of the present invention. - Certain terminology is used in the following description for convenience only and is not limiting. The words “lower,” “bottom,” “upper,” and “top” designate directions in the drawings to which reference is made. The words “inwardly,” “outwardly,” “upwardly” and “downwardly” refer to directions toward and away from, respectively, the geometric center of the device, and designated parts thereof, in accordance with the present disclosure. Unless specifically set forth herein, the terms “a,” “an” and “the” are not limited to one element, but instead should be read as meaning “at least one.” The terminology includes the words noted above, derivatives thereof and words of similar import.
- Embodiments of the invention are directed to a man-portable drone barrier system comprising modular components that are easily transported to any desired location, quickly assembled with minimal tools, and raised to a desired height via helium balloons (or any other suitable lifting device(s) or method(s)). Once assembled and raised, the system creates a mesh fence in the air to entrap and/or entangle a drone that flies into or near the barrier.
- Referring now to
FIG. 1 , adrone barrier system 10 is illustrated in accordance with embodiments of the invention.Barrier system 10 comprises afirst barrier assembly 12 a and asecond barrier assembly 12 b. The first and second barrier assemblies are assembled together as described below to form a complete barrier system. While two barrier assemblies are shown and described herein, more than two assemblies could be assembled together (as described further below) in a modular fashion to form a wider barrier if desired. Eachbarrier assembly - The
first barrier assembly 12 a comprises amain trunk line 16 a affixed at one end (viaconnection point 40 a) to a lighter-than-air object, such as aballoon 14 a inflated with a lighter-than-air gas such as helium or hydrogen, and at the other end (viaconnection point 42 a) to asecuring device 18 a for anchoring or securing theassembly 12 a to the ground (or to any other suitable fixed object), such as a ground stake, sandbag (or other similar weighted object), clamp, hook, carabiner, tie-off, or the like. Themain trunk line 16 a may be permanently affixed to theballoon 14 a, or may be removably affixed to theballoon 14 a such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation). Similarly, themain trunk line 16 a may be permanently affixed to the securingdevice 18 a, or may be removably affixed to the securingdevice 18 a such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation). - Similarly, the
second barrier assembly 12 b comprises amain trunk line 16 b affixed at one end (viaconnection point 40 b) to a lighter-than-air object, such as aballoon 14 b inflated with a lighter-than-air gas such as helium or hydrogen, and at the other end (viaconnection point 42 b) to a securingdevice 18 b for anchoring or securing theassembly 12 b to the ground (or to any other suitable fixed object), such as a ground stake, sandbag (or other similar weighted object), clamp, hook, carabiner, tie-off, or the like. Themain trunk line 16 b may be permanently affixed to theballoon 14 b, or may be removably affixed to theballoon 14 b such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation). Similarly, themain trunk line 16 b may be permanently affixed to the securingdevice 18 b, or may be removably affixed to the securingdevice 18 b such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation). - The
balloons assembly main trunk line - The
main trunk lines main trunk lines main trunk lines main trunk lines balloons securing devices main trunk lines main trunk lines balloons securing devices main trunk lines - The
first barrier assembly 12 a further comprises one or more (three are illustrated)branch lines 20 a affixed to the left side of themain trunk line 16 a in a spaced-apart configuration and one or more (three are illustrated)branch lines 20 a affixed to the right side of themain trunk line 16 a in a spaced-apart configuration. The left-side branch lines (and sub-branch lines, described below) of thefirst barrier assembly 12 a are typically (but not necessarily) identical to the right-side branch lines and sub-branch lines of thefirst barrier assembly 12 a, and are not fully illustrated for simplicity. (The left-side branch lines (and sub-branch lines) of thefirst barrier assembly 12 a may be omitted ifmain trunk line 16 a is to be the leftmost end of the barrier.) Typically (but not necessarily), the left-side and right-side branch and sub-branch lines of a given barrier assembly will be identical. Thebranch lines 20 a typically begin near the top end of themain trunk line 16 a (i.e., near theballoon 14 a) and extend lower at regular intervals until they reach a point at or near the connection between the main trunk line and the securing device, 18 a. Eachbranch line 20 a is affixed to themain trunk line 16 a at aconnection point 22 a. This connection point could be integral to the main trunk line as depicted or could be affixed with a clamp or simply by tying the branch line to the main trunk line. Eachbranch line 20 a may be permanently affixed to themain trunk line 16 a, or may be removably affixed to themain trunk line 16 a such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation including the simple tying of the branch line to the trunk line). Thebranch lines 20 a should be spaced close enough together for it to be unlikely that a drone could pass through the barrier, but far enough apart to provide the desired overall height of the barrier. In one exemplary embodiment of the invention, thebranch lines 20 a are spaced about eighteen inches apart. - Similarly, the
second barrier assembly 12 b further comprises one or more (three are illustrated)branch lines 20 b affixed to the left side of themain trunk line 16 b in a spaced-apart configuration and one or more (three are illustrated)branch lines 20 a affixed to the right side of themain trunk line 16 a in a spaced-apart configuration. The left-side branch lines (and sub-branch lines, described below) of thesecond barrier assembly 12 b are typically (but not necessarily) identical to the right-side branch lines and sub-branch lines of thesecond barrier assembly 12 b, and are not fully illustrated for simplicity. (The right-side branch lines (and sub-branch lines) of thesecond barrier assembly 12 b may be omitted ifmain trunk line 16 b is to be the rightmost end of the barrier.) Thebranch lines 20 b are typically located near the top end of themain trunk line 16 b (i.e., near theballoon 14 b) and extend lower at regular intervals until they reach a point at or near the connection between the main trunk line and the securing device, 18 b. (The branch lines should be affixed or affixable to each respective main trunk line at similar locations such that the branch lines attached to respective adjacent main trunk lines are properly aligned when the branch lines are connected as described below.) Eachbranch line 20 b is affixed to themain trunk line 16 b at aconnection point 22 b. This connection point could be integral to the main trunk line as depicted or could be affixed with a clamp or simply by tying the branch line to the main trunk line. Eachbranch line 20 b may be permanently affixed to themain trunk line 16 b, or may be removably affixed to themain trunk line 16 b such as via a hook on one side and a ring on the other side (or any other suitable mechanism for removable affixation including the simple tying of the branch line to the trunk line). Thebranch lines 20 b should be spaced close enough together for it to be unlikely that a drone could pass through the barrier, but far enough apart to provide the desired overall height of the barrier. In one exemplary embodiment of the invention, thebranch lines 20 b are spaced about eighteen inches apart. - The
branch lines branch lines trunk lines branch lines trunk lines branch lines branch lines trunk lines branch lines trunk lines - To assemble the
drone barrier system 10 illustrated inFIG. 1 , the distal end of one right-side branch line 20 a of thefirst assembly 12 a is affixed to the distal end of a corresponding left-side branch line 20 b of thesecond assembly 12 b atconnection point 24. The affixation of the distal ends is performed for each pair of corresponding branch lines from the right-side of thefirst assembly 12 a and the left-side of thesecond assembly 12 b. The distal ends of thecorresponding branch lines barrier system 10 comprising any desired number ofassemblies - Any desired number of barrier assemblies may be assembled together. For example, a third barrier assembly (not illustrated) may be connected to the
first barrier assembly 12 a on the opposite side from thesecond barrier assembly 12 b. To connect such a third barrier assembly, the right-side branch lines of the third assembly are affixed to the corresponding left-side branch lines 20 a of thefirst assembly 12 a. Similarly, a fourth barrier assembly (not illustrated) may be connected to thesecond barrier assembly 12 b on the opposite side from thefirst barrier assembly 12 a. To connect such a fourth barrier assembly, the left-side branch lines of the fourth assembly are affixed to the corresponding right-side branch lines 20 a of thesecond assembly 12 b. Many more additional barrier assemblies may be connected together as described to form a barrier system of a desired length. For the two barrier assemblies on the opposing ends of the completed barrier system, the branch lines that are not affixed to an adjacent assembly's branch lines may simply hang down. Alternatively, if the branch lines are removably affixed to the trunk lines, the branch lines that are not affixed to an adjacent assembly's branch lines may be removed. - The
first barrier assembly 12 a may further comprise one or more (six are illustrated)complete sub-branch lines 26 a and/or one or more partialsub-branch lines 28 a. Each completesub-branch line 26 a is affixed (permanently or removably) at opposing ends toadjacent branch lines 20 a, and together with thebranch lines 20 a form a grid and help maintain the spacing between thebranch lines 20 a. Because the complete sub-branch lines are affixed at opposing ends to adjacent branch lines, the complete sub-branch lines may also be termed “connecting lines.” Each partialsub-branch line 28 a is affixed (permanently or removably) at one end to a corresponding branch line, such that the opposing end is free and the partialsub-branch line 28 a swings freely. Because the partial sub-branch lines are affixed at only one end to a corresponding branch line, the partial sub-branch lines may also be termed “hanging lines.” - Similarly, the
second barrier assembly 12 b may further comprise one or more (six are illustrated)complete sub-branch lines 26 b and/or one or more partialsub-branch lines 28 b. Each completesub-branch line 26 b is affixed (permanently or removably) at opposing ends toadjacent branch lines 20 b, and together with thebranch lines 20 b form a grid and help maintain the spacing between thebranch lines 20 b. Each partialsub-branch line 28 b is affixed (permanently or removably) at one end to a corresponding branch line, such that the opposing end is free and the partialsub-branch line 28 b swings freely. - Each grid formed by the branch lines and the complete sub-branch lines and main trunk lines will typically have at least one and typically more than one partial sub-branch line positioned within the grid. In
FIG. 1 , most of the grids have one partial sub-branch line each and two of the grids have three sub-branch lines each. Any suitable number of partial sub-branch lines may be positioned within each grid, with any suitable spacing. Additionally, as shown inFIG. 1 , one ore more partialsub-branch lines - It is contemplated the partial sub-branch lines would be extremely light weight but high modulus (such as monofilament) such that they would entangle drone rotors either through gravity or by being pulled into the drone rotors through updraft (one of the partial
sub-branch lines 28 a is shown pulled upward as if by updraft). The completesub-branch line sub-branch lines sub-branch lines branch lines sub-branch lines branch lines - In alternative embodiments of the invention, the
complete sub-branch lines branch lines - The
complete sub-branch lines complete sub-branch lines sub-branch lines sub-branch lines complete sub-branch lines branch lines FIG. 1 , most of the partial sub-branch lines are the same length, but two of the grids are shown with three sub-branch lines each (including partialsub-branch lines - The free-swinging partial
sub-branch lines sub-branch line FIG. 1 in the top rightpartial sub-branch 28 a of thefirst assembly 12 a) and advantageously become entangled in one or more of the drone's rotors, thereby potentially disabling the drone. - After the distal ends of the
corresponding branch lines balloons 14, 14 b are inflated with a helium or hydrogen. The inflated balloons will rise to a height permitted by the length of themain trunk lines balloons main trunk lines branch lines main trunk lines main trunk lines branch lines complete sub-branch lines main trunk lines branch liens complete sub-branch lines sub-branch lines - In one exemplary embodiment of the invention, the trunk lines, branch lines, and complete sub-branch lines are made from AmSteel Blue rope from Samson Rope Technologies, Inc. which is made of Dyneema ultra-high-molecular-weight polyethylene (UHMWPE). The trunk is 5/32″ diameter with a 4000 pound (lb.) average strength, and the branches are 7/64″ diameter with a 1600 lb. average strength. The partial sub-branch lines are made of 25 lb. monofilament fishing line from Ande, Inc.
- The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof.
- The corresponding structures, materials, acts, and equivalents of all means or step plus function elements in the claims below are intended to include any structure, material, or act for performing the function in combination with other claimed elements as specifically claimed. The description of the present invention has been presented for purposes of illustration and description, but is not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the invention. The embodiment was chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.
Claims (19)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
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US15/928,318 US20190041170A1 (en) | 2017-08-01 | 2018-03-22 | Modular man-portable drone barrier |
CN201880050638.2A CN110998220A (en) | 2017-08-01 | 2018-07-16 | Modular single portable unmanned aerial vehicle barrier |
PCT/US2018/042285 WO2019027665A1 (en) | 2017-08-01 | 2018-07-16 | Modular man-portable drone barrier |
IL272127A IL272127A (en) | 2017-08-01 | 2020-01-19 | Modular man-portable drone barrier |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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US201762539608P | 2017-08-01 | 2017-08-01 | |
US15/928,318 US20190041170A1 (en) | 2017-08-01 | 2018-03-22 | Modular man-portable drone barrier |
Publications (1)
Publication Number | Publication Date |
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US20190041170A1 true US20190041170A1 (en) | 2019-02-07 |
Family
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US15/928,318 Pending US20190041170A1 (en) | 2017-08-01 | 2018-03-22 | Modular man-portable drone barrier |
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US (1) | US20190041170A1 (en) |
CN (1) | CN110998220A (en) |
IL (1) | IL272127A (en) |
WO (1) | WO2019027665A1 (en) |
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RU2721815C1 (en) * | 2019-04-08 | 2020-05-22 | Акционерное общество Научно-производственный центр "Электронные вычислительно-информационные системы" | Anti-drone system |
RU191584U1 (en) * | 2019-04-08 | 2019-08-13 | Акционерное общество Научно-производственный центр "Электронные вычислительно-информационные системы" | RESISTANCE SYSTEM FOR UNMANNED AERIAL VEHICLES |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH71208A (en) * | 1915-09-13 | 1915-12-01 | Fraeulein Josty Fritza | Device to defend against enemy aircraft during the night |
GB538395A (en) * | 1939-10-05 | 1941-08-01 | Joseph Francis Leeson Mccann | Apparatus for countering raiding aircraft |
GB545611A (en) * | 1940-12-28 | 1942-06-04 | John Pinder | Improvements in and relating to balloon-supported net and like obstructions against hostile aircraft |
US2365778A (en) * | 1941-09-16 | 1944-12-26 | Martin C Schwab | Mobile device for repelling the attack of enemy aircraft |
US8038097B1 (en) * | 2007-12-05 | 2011-10-18 | Lockheed Martin Corporation | Vehicle recovery package |
ITRM20080235A1 (en) * | 2008-05-05 | 2009-11-06 | Gianni Petrangeli | SYSTEM FOR THE EXTERNAL PROTECTION OF PLANTS FROM THE FALL OF PLANES |
US8434711B2 (en) * | 2008-12-31 | 2013-05-07 | Joel F. Berman | Unguided missile and projectile defense shield supported by tethered balloons |
US9228807B1 (en) * | 2013-02-11 | 2016-01-05 | Lockheed Martin Corporation | Anti-ship cruise missile barrier |
GB2538826B (en) * | 2015-04-22 | 2021-06-23 | Openworks Eng Ltd | System for deploying a first object for capturing, immobilising or disabling a second object |
GB2538976B (en) * | 2015-06-01 | 2021-07-28 | David Down Christopher | Net for tangling the rotating elements of a vehicle |
CN106767172B (en) * | 2017-01-23 | 2018-04-03 | 芜湖博高光电科技股份有限公司 | A kind of pickaback portable anti-unmanned aerial vehicle ejecting is soft to injure retracting device |
-
2018
- 2018-03-22 US US15/928,318 patent/US20190041170A1/en active Pending
- 2018-07-16 CN CN201880050638.2A patent/CN110998220A/en active Pending
- 2018-07-16 WO PCT/US2018/042285 patent/WO2019027665A1/en active Application Filing
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2020
- 2020-01-19 IL IL272127A patent/IL272127A/en unknown
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WO2019027665A1 (en) | 2019-02-07 |
IL272127A (en) | 2020-03-31 |
CN110998220A (en) | 2020-04-10 |
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